How to Calculate Pressure Coefficient for Slender Bodies of Revolution?
Pressure Coefficient for Slender Bodies of Revolution calculator uses Pressure Coefficient = 2*(Angle of Inclination)^2+Curvature of Surface*Distance of Point from Centroidal Axis to calculate the Pressure Coefficient, Pressure Coefficient for Slender Bodies of Revolution formula is defined as a measure of the aerodynamic efficiency of slender bodies in hypersonic flow, reflecting the relationship between pressure variations and the body's curvature and angle of attack. Pressure Coefficient is denoted by Cp symbol.
How to calculate Pressure Coefficient for Slender Bodies of Revolution using this online calculator? To use this online calculator for Pressure Coefficient for Slender Bodies of Revolution, enter Angle of Inclination (θ), Curvature of Surface (kc) & Distance of Point from Centroidal Axis (y) and hit the calculate button. Here is how the Pressure Coefficient for Slender Bodies of Revolution calculation can be explained with given input values -> 0.302148 = 2*(0.55850536063808)^2+0.2*1.2.